Epicyclical gear system housing assembly

Patent metadata

Field	Value
Publication number	US-11353089-B2
Application number	US-201916592492-A
Country	US
Kind code	B2
Filing date	Oct 3, 2019
Priority date	Oct 3, 2019
Publication date	Jun 7, 2022
Grant date	Jun 7, 2022

Abstract

A planet gear housing assembly is disclosed in an epicyclical gear system of a gas turbine engine. The planet gear housing assembly comprises an aft planet carrier assembly, a forward planet carrier assembly, and a plurality of planet gears. The planet gear housing assembly includes one or more of the following features: a stiffening member positioned between the forward and aft planet carrier assemblies, a static curvic joint coupling the forward and aft planet carrier assemblies, a plurality of roller element bearings to carry the plurality of planet gears, and one or more bearing springs disposed between a bearing and a carrier housing to accommodate relative movement.

First claim

What is claimed is:

1. A planet gear housing assembly in an epicyclical gear assembly comprising:
an aft planet carrier assembly comprising an aft flange defining a central aperture and a plurality of gear shaft pockets positioned about the circumference and radially outward of said central aperture, each pocket having a cylindrical wall;
a forward planet carrier assembly comprising a forward flange defining a central aperture and a plurality of gear shaft pockets positioned about the circumference and radially outward of said central aperture, each pocket having a cylindrical wall;
a plurality of planet gears each comprising a cylindrical shaft having a forward end portion disposed in a gear shaft pocket of said forward planet carrier assembly coaxially with the cylindrical wall of said pocket, an aft end portion disposed within a gear shaft pocket of said aft planet carrier assembly coaxially with the cylindrical wall of said pocket, and one or more gears carried by said shaft between said forward and aft end portions;
a bearing assembly comprising:
a bearing disposed over at least a portion of one of the aft end portion and the forward end portion of said gear shaft; and
an annular spring disposed over at least a portion of said bearing;

and
a stiffening member positioned between said aft planet carrier assembly and said forward planet carrier assembly, said stiffening member comprising:
an annular body defining a central aperture; and
a plurality of radial flanges extending radially outward from said annular body, each of said plurality of radial flanges partly defining a gear-facing surface.

2. The planet gear housing assembly of claim 1 wherein said bearing is a roller bearing.

3. The planet gear housing assembly of claim 1 wherein said shaft and gears form a compound star gear in an epicyclical gear system.

4. The planet gear housing assembly of claim 1 wherein said annular spring comprises an annular body and a plurality of mutes spaced about a circumference of said body.

5. The planet gear housing assembly of claim 1 wherein said aft planet carrier assembly is coupled to said forward planet carrier assembly.

6. The planet gear housing assembly of claim 5 :
wherein said aft planet carrier assembly further comprises an annular mounting flange extending from said aft flange, said annular mounting flange positioned forward of and coaxial with said central aperture, said mounting flange forming a forward facing mounting surface comprising a curvic structure;
wherein said forward planet carrier assembly further comprises an annular mounting flange extending from said forward flange, said annular mounting flange positioned aft of and coaxial with said central aperture, said mounting flange forming an aft facing mounting surface comprising a curvic structure; and
wherein said mounting surfaces are positioned relative to each other to thereby form a static curvic joint.

7. The planet gear housing assembly of claim 1 wherein each of said plurality of planet gears comprise a sun gear engaging gear and a ring gear engaging gear carried by said shaft between said forward and aft end portions.

8. A planet gear housing assembly in an epicyclical gear assembly comprising:
an aft planet carrier assembly comprising:
an aft flange defining a central aperture and a plurality of gear shaft pockets positioned about the circumference and radially outward of said central aperture, each pocket having a cylindrical wall; and
an annular mounting flange positioned forward of and coaxial with said central aperture, said mounting flange forming a forward facing mounting surface comprising a curvic structure;

a forward planet carrier assembly comprising:
a forward flange defining a central aperture and a plurality of gear shaft pockets positioned about the circumference and radially outward of said central aperture, each pocket having a cylindrical wall; and
an annular mounting flange positioned aft of and coaxial with said central aperture, said mounting flange forming an aft facing mounting surface comprising a curvic structure;

a plurality of planet gears each comprising a cylindrical shaft having a forward end portion disposed in a gear shaft pocket of said forward planet carrier assembly coaxially with the cylindrical wall of said pocket, an aft end portion disposed within a gear shaft pocket of said aft planet carrier assembly coaxially with the cylindrical wall of said pocket, and one or more gears carried by said shaft between said forward and aft end portions; and
a stiffening member positioned between said aft planet carrier assembly and said forward planet carrier assembly, said stiffening member comprising:
an annular body defining a central aperture; and
a plurality of radial flanges extending radially outward from said annular body, each of said plurality of radial flanges partly defining a gear-facing surface;

wherein said curvic structures of said mounting surfaces are positioned relative to each other to thereby form a static curvic joint.

9. The planet gear housing assembly of claim 8 wherein said shaft and gears form a compound star gear in an epicyclical gear system.

10. The planet gear housing assembly of claim 8 wherein said epicyclical gear assembly is a portion of a gas turbine engine having an engine casing, and wherein said aft flange is coupled to said engine casing to define an aft torsional stiffness and said forward flange is coupled to said aft planet housing assembly to define a forward torsional stiffness, and wherein said forward torsional stiffness is between 60% and 80% of the aft torsional stiffness.

11. The planet gear housing assembly of claim 10 wherein said forward torsional stiffness is between 65% and 75% of the aft torsional stiffness.

12. The planet gear housing assembly of claim 8 further comprising:
a bearing assembly comprising:
a roller bearing disposed over at least a portion of one of the aft end portion and the forward end portion of said gear shaft; and
an annular spring disposed over at least a portion of said bearing.

13. The planet gear housing assembly of claim 12 wherein said annular spring comprises an annular body and a plurality of mutes spaced about a circumference of said body.

Assignees

• Rolls Royce Corp

Inventors

• Bennett Brian
• Winely Mark

Classifications

• F16H2057/085

  Bearings for orbital gears · CPC title

• F16H57/082 Primary

  Planet carriers · CPC title

• F02C7/36

  Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user ({F02C3/107 - F02C3/13 and} F02C7/32 take precedence; couplings for transmitting rotation F16D; gearing in general F16H) · CPC title

• F16H57/08

  of gearings with members having orbital motion · CPC title

• F16H1/2863 Primary

  Arrangements for adjusting or for taking-up backlash · CPC title